elevator
The control surface that controls pitch is the elevator. It is located on the horizontal stabilizer of an aircraft and is used to control the aircraft's pitch attitude by adjusting the angle of the stabilizer.
No, the rudder does not control the pitch of an aircraft. The rudder is primarily used for controlling yaw, which is the side-to-side movement of the aircraft's nose. Pitch is controlled by the elevator, which is located on the tail of the aircraft and adjusts the angle of the plane's nose up or down.
Elevators control the pitch (up and down) of the aircraft. Ailerons control the roll of the aircraft. And rudders control the yaw of the aircraft.
The elevator is the longitudinal control surface on an aircraft. It is located on the horizontal stabilizer and is used to control the pitch motion of the aircraft, which refers to the up and down movement of the nose.
Elevators are flight control surfaces, usually at the rear of an aircraft, which control the aircraft's pitch
Pitch controls the angle up or down of the aircraft.
It is a tool used to manualy change the pitch of an variable pitch aircraft propeller.
Elevators. They control the pitch of the aircraft.
The ailerons are used to control roll rate. The flaps are used to increase lift at slow speeds. The elevators are use to control pitch. The rudder is used to control yaw. The spoilers are used to slow the aircraft quickly. The trim tabs are used to adjust back pressure to achieve straight and level flight with no control input.
Aircraft have two controls that are used together to control altitude.The elevator is used to increase the nose up pitch of the aircraft and it starts to climbThe throttle must then be increased so the air craft will continue at the speed needed to climbThe throttle can be used only in some aircraft but it is not a real stable usable thing, the elevator must be used to stabilise the aircraftTo descend oer maintain altitude the same controls are used together.
no No, they do not control speed. Elevators are flight control surfaces, usually at the rear of an aircraft, which control the aircraft's longitudinal attitude by changing the pitch balance, and so also the angle of attack and the lift of the wing.
The control surfaces, rudder, elevators and ailerons.